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| Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
Authors: Yang F(杨帆); Lin MY(林明月); Hu ZM(胡宗民) ; Han GL(韩桂来)
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oblique detonation engine cantilevered injection localized high heat flux boundary layer separation reattachment |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | Favorite | View/Download：356/178 | Submit date：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林)
Adobe PDF(2818Kb) | Favorite | View/Download：315/119 | Submit date：2021/01/29
Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒)
Adobe PDF(1090Kb) | Favorite | View/Download：278/101 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors: Yuan CK(苑朝凯); Zhou K(周凯); Hu ZM(胡宗民); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1471Kb) | Favorite | View/Download：260/60 | Submit date：2020/07/06 |
| Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684
Authors: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民); Deng, X
Adobe PDF(2321Kb) | Favorite | View/Download：357/88 | Submit date：2019/10/21
Oblique detonation wave Blunt wedge Initiation Hydrogen |
| Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 卷号: 44, 期号: 41, 页码: 23429-23435
Authors: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民)
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Oblique detonation wave Boundary layer Viscosity Detonation initiation Hydrogen-air mixture |
| Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors: Luo ZT(罗长童); Wang YP(汪运鹏); Hu ZM(胡宗民); Li JP(李进平); Jiang ZL(姜宗林)
View | Adobe PDF(2227Kb) | Favorite | View/Download：285/68 | Submit date：2019/10/21
Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
View | Adobe PDF(2165Kb) | Favorite | View/Download：421/98 | Submit date：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| Hypervelocity Test with a Detonation-Driven Expansion Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Hu ZM(胡宗民); Zhou K(周凯); Peng J(彭峻); Jiang ZL(姜宗林)
View | Adobe PDF(297Kb) | Favorite | View/Download：214/72 | Submit date：2020/01/06 |
